View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 27387U 02009B 23028.52800181 .00000144 00000-0 64808-4 0 9997
2 27387 98.7437 4.4400 0032448 172.0531 188.1175 14.36130691 95918
Epoch (UTC): | 28 January 2023 12:40:19 |
Eccentricity: | 0.0032448 |
inclination: | 98.7437° |
perigee height: | 748 km |
apogee height: | 794 km |
right ascension of ascending node: | 4.4400° |
argument of perigee: | 172.0531° |
revolutions per day: | 14.36130691 |
mean anomaly at epoch: | 188.1175° |
orbit number at epoch: | 9591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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